EP2342428A2 - Turbocompresseur à double entrée - Google Patents
Turbocompresseur à double entréeInfo
- Publication number
- EP2342428A2 EP2342428A2 EP09778487A EP09778487A EP2342428A2 EP 2342428 A2 EP2342428 A2 EP 2342428A2 EP 09778487 A EP09778487 A EP 09778487A EP 09778487 A EP09778487 A EP 09778487A EP 2342428 A2 EP2342428 A2 EP 2342428A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- exhaust gas
- turbine
- channel
- turbine housing
- twinscroll
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 238000002485 combustion reaction Methods 0.000 claims abstract description 11
- 238000010438 heat treatment Methods 0.000 claims description 10
- 239000002826 coolant Substances 0.000 claims description 8
- 239000007769 metal material Substances 0.000 claims description 5
- 229910052782 aluminium Inorganic materials 0.000 claims description 3
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 3
- 238000013021 overheating Methods 0.000 description 6
- 229910052751 metal Inorganic materials 0.000 description 4
- 239000002184 metal Substances 0.000 description 4
- 230000008901 benefit Effects 0.000 description 3
- 239000003054 catalyst Substances 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 230000000694 effects Effects 0.000 description 1
- 238000010304 firing Methods 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 239000007858 starting material Substances 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B39/00—Component parts, details, or accessories relating to, driven charging or scavenging pumps, not provided for in groups F02B33/00 - F02B37/00
- F02B39/005—Cooling of pump drives
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/08—Cooling; Heating; Heat-insulation
- F01D25/14—Casings modified therefor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/026—Scrolls for radial machines or engines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
- F02B37/02—Gas passages between engine outlet and pump drive, e.g. reservoirs
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
- F02B37/02—Gas passages between engine outlet and pump drive, e.g. reservoirs
- F02B37/025—Multiple scrolls or multiple gas passages guiding the gas to the pump drive
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2220/00—Application
- F05D2220/40—Application in turbochargers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2300/00—Materials; Properties thereof
- F05D2300/10—Metals, alloys or intermetallic compounds
- F05D2300/12—Light metals
- F05D2300/121—Aluminium
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
Definitions
- the invention relates to a twin-scroll turbocharger with the features of the preamble of patent claim 1.
- twin-scroll turbocharger for a multi-cylinder internal combustion engine.
- the twinscroll exhaust gas turbocharger has a turbine housing with first and second intake passages separated by the turbine housing. Both inlet channels open in each case into a first and a second spiral channel, which extend radially outward, largely parallel to one another about a rotatably mounted exhaust gas turbine. Both intake ports are acted upon by exhaust gas of different cylinders of the internal combustion engine in accordance with the firing order of the internal combustion engine, whereby a more uniform drive of the exhaust gas turbine takes place.
- the gas inlet channels and the spiral channels are arranged such that the exhaust gas is passed from opposite sides to the exhaust gas turbine.
- a disadvantage of the known design is a high temperature load of the turbine housing, in particular in the region of the spiral channels.
- the turbine housing can be made in a further particularly preferred embodiment of a light metal material, in particular aluminum.
- a light metal material in particular aluminum.
- the sealing problem is significantly simplified in an embodiment according to claim 3, as a simpler thermal connection of the exhaust gas turbocharger to the cylinder head and the crankcase is possible if they are also made of a light metal material (same or similar thermal expansion coefficient).
- the embodiment according to claim 4 is used for heating the turbine housing after a cold start of the internal combustion engine, whereby the energy loss is reduced in the catalyst heating.
- the recuperated energy from the battery of a mild hybrid can be used.
- the heating element according to claim 5 is a particularly preferred heating element.
- Fig. 1 shows the top view of a wireframe model of gas leading
- FIG. 1 shows a three-dimensional plan view of a wire grid model of gas-carrying channels for a twinscroll exhaust gas turbocharger according to the invention for an internal combustion engine. Shown in the wireframe model are a first gas inlet channel 1 and a second gas inlet channel 1 ', wherein the first gas inlet channel merges into a first spiral channel 2 and the second gas inlet channel 1' into a second spiral channel 2 '. Of the two spiral channels 2, 2 'an exhaust gas turbine chamber 5 is largely enclosed, in which an exhaust gas turbine, not shown, can be arranged. An axis of rotation of the exhaust turbine is numbered 3.
- spiral channels wrap around the exhaust gas turbine chamber 5 radially outward, each with a wrap angle smaller than 180 °, wherein the spiral channels 2, 2 'are not arranged parallel to each other.
- the gas inlet ducts 1, 1 ' at least partially parallel to each other in the turbine housing, not shown, and arranged radially spaced from each other with respect to the rotation axis 3.
- the first spiral channel 2, which adjoins the closer to the axis of rotation 3 arranged first gas inlet channel 1 extends almost 180 ° to the exhaust gas turbine.
- the second spiral channel 2 ', which adjoins the second gas inlet channel V, which is farther from the rotation axis 3, extends largely around the remaining circumference around the exhaust gas turbine.
- a meaningful wrap angle of the spiral channels 2, 2 'around the exhaust gas turbine chamber 5 is between 90 ° and 180 °, so that no intersection of the spiral channels 2, 2' takes place.
- the turbine housing has at least one coolant channel (not shown in FIG. 1), at least between the gas inlet channels 1, 1 ', through which a coolant can flow.
- a coolant may be, for example, a liquid or gaseous coolant.
- the liquid coolant used is preferably a combustion engine-own coolant. Cooling with air is also possible. By this measure, overheating of the turbine housing is further reduced.
- a heating element preferably a PTC (positive temperat ⁇ re coefficient) are arranged.
- PTC positive temperat ⁇ re coefficient
- This measure serves to heat the turbine housing after a cold start of the internal combustion engine and thus leads to a reduction of the energy loss during catalyst heating.
- the recuperated energy from the battery of a mild hybrid, as defined above, can be used for this purpose.
- a water-cooled twinscroll exhaust-gas turbocharger can be represented, for example, with a wastegate.
- the inventive design leads to a reduction in the weight of the exhaust gas turbocharger and the cost, since cheaper materials, such as light metal materials for the manufacture of the turbine housing can be used.
- a simpler thermal connection of the exhaust gas turbocharger to achtmetali cylinder head or a light metal crankcase due to the same or similar thermal expansion coefficients is possible.
- the seal between a light metal cylinder head or a light metal crankcase and a light metal turbine housing is much less critical with respect to thermal distortion and thus leaks.
- Another advantage is the lower heat input into the engine compartment to mention, so that the heat protection measures in the engine compartment can be reduced, which also creates a cost and weight advantage.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Supercharger (AREA)
Abstract
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102008056358A DE102008056358A1 (de) | 2008-11-07 | 2008-11-07 | Twinscroll-Abgasturbolader |
PCT/EP2009/006612 WO2010051876A2 (fr) | 2008-11-07 | 2009-09-11 | Turbocompresseur à double entrée |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2342428A2 true EP2342428A2 (fr) | 2011-07-13 |
EP2342428B1 EP2342428B1 (fr) | 2014-06-25 |
Family
ID=42096413
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP09778487.0A Active EP2342428B1 (fr) | 2008-11-07 | 2009-09-11 | Turbocompresseur à double entrée |
Country Status (4)
Country | Link |
---|---|
US (1) | US8333550B2 (fr) |
EP (1) | EP2342428B1 (fr) |
DE (1) | DE102008056358A1 (fr) |
WO (1) | WO2010051876A2 (fr) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR101678010B1 (ko) * | 2009-09-10 | 2016-11-21 | 보르그워너 인코퍼레이티드 | 배기가스 터보차저의 터빈 휠의 배기가스 공급 장치 |
JP5609795B2 (ja) * | 2011-07-12 | 2014-10-22 | 株式会社デンソー | 車両用過給装置 |
US9828913B2 (en) | 2013-08-16 | 2017-11-28 | Wescast Industries, Inc. | Turbine housing |
JP6315020B2 (ja) * | 2016-04-05 | 2018-04-25 | トヨタ自動車株式会社 | 内燃機関 |
US10662904B2 (en) | 2018-03-30 | 2020-05-26 | Deere & Company | Exhaust manifold |
US11073076B2 (en) | 2018-03-30 | 2021-07-27 | Deere & Company | Exhaust manifold |
DE102018209078A1 (de) | 2018-06-07 | 2019-06-13 | Audi Ag | Turbine für einen Abgasturbolader, Abgasturbolader für eine Antriebseinrichtung sowie entsprechende Antriebseinrichtung |
US20220412221A1 (en) * | 2021-06-23 | 2022-12-29 | International Engine Intellectual Property Company, Llc | Multiple Scroll Entry Turbine Turbocharger |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2384251A (en) * | 1943-01-14 | 1945-09-04 | Wright Aeronautical Corp | Liquid cooled supercharger |
US2861774A (en) * | 1950-02-16 | 1958-11-25 | Alfred J Buchi | Inlet control for radial flow turbines |
US3010697A (en) * | 1958-06-16 | 1961-11-28 | Thompson Ramo Wooldridge Inc | Turbocharger |
JPS57137619A (en) * | 1981-02-18 | 1982-08-25 | Hitachi Ltd | Exhaust bypass device of turbocharger for multi- cylinder engine |
JPH03151519A (ja) | 1989-11-08 | 1991-06-27 | Toyota Motor Corp | ターボチャージャ付多気筒エンジン |
US5340286A (en) * | 1990-10-29 | 1994-08-23 | Wojceich Kanigowski | Balanced turbocharger |
DE4242494C1 (en) * | 1992-12-16 | 1993-09-09 | Mercedes-Benz Aktiengesellschaft, 70327 Stuttgart, De | Adjustable flow-guide for engine exhaust turbocharger - has axially-adjustable annular insert in sectors forming different kinds of guide grilles supplied simultaneously by spiral passages |
DE19653057A1 (de) * | 1996-12-19 | 1998-06-25 | Asea Brown Boveri | Radialturbine eines Turboladers |
DE50303860D1 (de) * | 2003-11-28 | 2006-07-27 | Borgwarner Inc | Gehäuse für Turbolader |
FR2878562B1 (fr) * | 2004-11-30 | 2007-04-06 | Renault Sas | Organe d'echappement d'un moteur a combustion interne de vehicule automobile pourvu d'un dispositif de chauffage |
WO2007035972A2 (fr) * | 2005-09-27 | 2007-04-05 | Avl List Gmbh | Moteur a combustion interne a suralimentation a deux etages |
DE102007034235A1 (de) * | 2007-07-23 | 2009-01-29 | Continental Automotive Gmbh | Strömungsgehäuse eines Turboladers |
-
2008
- 2008-11-07 DE DE102008056358A patent/DE102008056358A1/de not_active Withdrawn
-
2009
- 2009-09-11 WO PCT/EP2009/006612 patent/WO2010051876A2/fr active Application Filing
- 2009-09-11 EP EP09778487.0A patent/EP2342428B1/fr active Active
-
2011
- 2011-05-06 US US13/102,607 patent/US8333550B2/en active Active
Non-Patent Citations (1)
Title |
---|
See references of WO2010051876A2 * |
Also Published As
Publication number | Publication date |
---|---|
EP2342428B1 (fr) | 2014-06-25 |
US20110236198A1 (en) | 2011-09-29 |
US8333550B2 (en) | 2012-12-18 |
WO2010051876A2 (fr) | 2010-05-14 |
WO2010051876A3 (fr) | 2011-03-24 |
DE102008056358A1 (de) | 2010-05-12 |
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